Beechcraft Baron G58 Pilot Operating Handbook page 173

Model G58
2. COCKPIT
a. Landing Gear Emergency Handcrank . . . . STOWED
b. Fire Extinguisher . . . . . . . . . . . . . . . . . . . . . . CHECK
c. Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
d. Control Locks . . . . . . . . . . . . . . . . . . . . . . . REMOVE
e. All Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
f. Landing Gear Handle . . . . . . . . . . . . . . . . . . . .DOWN
g. Trim Tabs . . . . . . . . . . . . . . . . . . . . . . SET TO ZERO
h. Battery System. . . . . . . . . . . . . . . . . . . . . . . . CHECK
1) L BAT and R BAT . . . . . . . . . . . . . . . . . . . . . . .ON
2) PFD . . . . . . . . . VERIFY REVERSIONARY MODE
3) Soft Keys . . . . . . . . SELECT ENGINE & SYSTEM
4) L Bus & R Bus Voltages . . . . . . . . . . . . . . CHECK
a) L Bus = 23 Volts minimum
b) R Bus = 23 Volts minimum
i. Landing Gear Position Lights . . . . .CHECK 3 GREEN
j. Annunciator Test Button . . . . . . . . . . . . . . . . PRESS
• Gear In-Transit Light and
Flap Lights. . . . . . . . . . . . . . . . . . . . . ILLUMINATED
k. Exterior/Interior Lights . . . . .CHECK, AS REQUIRED
l. Standby Attitude Indicator . . . . . . . . . FLAG PULLED
m. L BAT & R BAT . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
n. Standby Attitude Indicator . . . . . . . . . . YELLOW LED
• Will automatically shutdown after 1 minute
3. RIGHT FUSELAGE
• Static Port . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
April, 2008
Section 4
Normal Procedures
AND ACCESSIBLE
BLINKING
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